Please use this identifier to cite or link to this item: http://er.nau.edu.ua/handle/NAU/22133
Full metadata record
DC FieldValueLanguage
dc.contributor.authorKulik M.S.-
dc.contributor.authorAntonov V.K.-
dc.contributor.authorGlazok O.M.-
dc.contributor.authorOlefir O.I.-
dc.contributor.authorГлазок, Олексій Михайлович-
dc.contributor.authorГлазок О.М.-
dc.contributor.authorГлазок, Алексей Михайлович-
dc.contributor.authorГлазок А.М.-
dc.date.accessioned2016-08-02T13:22:31Z-
dc.date.available2016-08-02T13:22:31Z-
dc.date.issued2015-10-
dc.identifier.citationUnmanned aircraft with a closed wing /M.S.Kulik, V.K.Antonov, O.M.Glazok, O.I.Olefir //Proceedings of the 2015 IEEE 3rd International Conference "Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)" October 13-15, 2015. Kyiv, Ukraine. – Pp. 54-58.uk_UA
dc.identifier.isbn978-1-4673-6566-6-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/22133-
dc.descriptionhttp://ieeexplore.ieee.org/xpl/login.jsp?tp=&arnumber=7346558&url=http%3A%2F%2Fieeexplore.ieee.org%2Fxpls%2Ficp.jsp%3Farnumber%3D7346558uk_UA
dc.description.abstractA configuration of an unmanned aircraft with closed wing is considered. The method of identification designed for researching the aerodynamic qualities of the model is proposed.uk_UA
dc.language.isoen_USuk_UA
dc.publisherIEEEuk_UA
dc.subjectunmanned aircraftuk_UA
dc.subjectclosed winguk_UA
dc.subjectautomatic controluk_UA
dc.subjectidentificationuk_UA
dc.subjectauxiliary equationuk_UA
dc.subjectsimulatoruk_UA
dc.titleUnmanned aircraft with a closed winguk_UA
dc.typeOtheruk_UA
Appears in Collections:Тези доповідей кафедри КСУ



Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.